NASA NTRS · 20180002524
Non-Axisymmetric Fixed or Variable Fan Nozzle for Boundary Layer Ingestion Propulsion
Abstract
A fan section for an engine has a fan which rotates about an axis, the fan has an inlet for ingesting ambient air, and a non-axisymmetric nozzle for providing the fan with non-uniform back pressure.
Keep this discovery
Explore connections, maps & timelines
Tillman, Thomas G, Lord, Wesley K.. 2018-03-06. Non-Axisymmetric Fixed or Variable Fan Nozzle for Boundary Layer Ingestion Propulsion. https://ntrs.nasa.gov/citations/20180002524
Cite the original work for its findings. Save a collection to share your selection of sources.